Your opinion is arbitrary. My drag coefficient used is based on facts. The missile diameter is the same as the AIM-7F. The drag coefficients in-game are pretty linear and affected by more than just the number. They are affected by caliber.
The R-77 has slightly smaller diameter irl, and the same in-game (200mm). Lower drag wings, and the point of contention is on the grid fins. Using the same coefficient as the AIM-7F is actually quite conservative imo. If you think otherwise we can probably math it out once the CFD is done by the DCS devs. Until then, I’m inclined to believe that the drag coefficient I used netted a conservative analysis of the data.
Heck, I can even test the missile with the obscenely higher R-23R drag coefficient of 2.55 (vs 2.3 for AIM-7F and 2.1 for R-24R). I’ll even test it at an arbitrarily huge number like 2.75.
Iteration 1 test, 2.3 drag coefficient (75km in ~79s) Direct impact.
Iteration 2 test, 2.55 drag coefficient (75km in ~80s) Direct impact.
Iteration 3 test, 2.75 drag coefficient (75km in ~80s) Direct impact.
Iteration 4 test, 3.0 drag coefficient (75km in ~80s) Direct impact.
Seems that Gaijin models very little drag at altitudes of 15km (crazy, I know). Could be other issues with the testing though if there is an issue. I saw the edit to your last post about the CxK and I can do further testing with 3-3.5 CxK though I really doubt it could be that high as the average would be lower due to the reduced drag during periods above mach 2 in comparison.
Also, a reminder that I have yet to adjust the thrust to account for the reduction in drag during burn time. Do you have a recommendation for how much the motor would reduce drag during burn time so I can adjust the thrust?
-edit- I have added the 3.0 drag coefficient test.